Lidar-Based Safe Site Relative NavigationThere has been a renewed focus in exploration of the lunar surface and maximizing scientific potential of such missions is made possible in part by minimizing the time required to set up operations; that is, reducing transit time on the surface by increasing the landing precision with respect to the intended target. Established SPLICE project precision landing requirements necessitate a navigation filter architecture and underlying models developed specifically with these needs in mind. To date, test flights to characterize SPLICE GNC system performance have not provided a means to divert from the a priori selected landing site due to hazardous conditions. With the inclusion of a new sensor, the HDL, coupled with safe landing site selection algorithms, GNC can divert from the originally planned trajectory and navigate relative to the new targeted landing site. This work presents a novel hazard relative measurement model and covariance transformation methodology that enable the navigation system to inform a safe-site relative guidance profile to meet project precision landing goals.
Document ID
20230015916
Acquisition Source
Johnson Space Center
Document Type
Conference Paper
Authors
Kari C Ward (Draper Laboratory Cambridge, Massachusetts, United States)
Kyle W Smith (Draper Laboratory Cambridge, Massachusetts, United States)
Isaac S Rowe (Jacobs (United States) Dallas, Texas, United States)
Jeanette M Harper (Odyssey Space Research (United States) Houston, Texas, United States)
Davis W Adams (Johnson Space Center Houston, Texas, United States)
Samuel M Pedrotty (Johnson Space Center Houston, Texas, United States)
Gavin F Mendeck (Johnson Space Center Houston, Texas, United States)
Date Acquired
November 3, 2023
Subject Category
Lunar and Planetary Science and ExplorationStatistics and ProbabilitySpacecraft Design, Testing and Performance
Meeting Information
Meeting: AIAA SciTech Forum
Location: Orlando, FL
Country: US
Start Date: January 8, 2024
End Date: January 12, 2024
Sponsors: American Institute of Aeronautics and Astronautics
Funding Number(s)
WBS: 335803.04.25.72
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
NASA Peer Committee
Keywords
NavigationEstimationSpacecraft Entry Descent and Landing